A study of screech tone noise of supersonic swirling jets

Journal of Sound and Vibration

Volumn 205, Issue 5, 1997, Pages 698-705

  Yu, Y K ^a   Chen, R H ^a  

^a University of Central Florida   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; ACOUSTIC WAVE TRANSMISSION; NOZZLES; PRESSURE EFFECTS; ROTATIONAL FLOW; SUPERSONIC FLOW;

QUASI PERIODIC SHOCK STRUCTURES; RECIRCULATION FLOW; SCREECH TONE NOISE; SHOCK CELLS; SUPERSONIC SWIRLING JETS;

JETS;

EID: 0031553021     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.1997.1027     Document Type: Editorial

References (13)

1. R. SMITH 1973 Aeronautical Quarterly, August, 167-178. An investigation of supersonic swirling jets.
2. P. W. CARPENTER 1985 American Institute of Aeronautics and Astronautics Journal 23, 1902-1909. A linearized theory of swirling supersonic jets and its application to shock-cell noise.
3. W. S. LEWELLEN, W. J. BURNS and H. J. STRICKLAND 1969 American Institute of Aeronautics and Astronautics Journal 7, 1290-1297. Transonic swirling flow.
4. R.-H. CHEN and J. F. DRISCOLL 1988 in Twenty-second Symposium (International) on Combustion, 531-540. Pittsburgh: The Combustion Institute. The role of the recirculation vortex in improving fuel-air mixing with in swirling flames.
5. R.-H. CHEN, J. F. DRISCOLL, J. KELLY, M. NAMAZIAN and R. SCHEFER 1990 Combustion Science and Technology 71, 197-217. A comparison of bluff-body and swirl-stabilized flames.
6. D. FEIKEMA, R.-H. CHEN and J. F. DRISCOLL 1990 Combusion and Flame 80, 183-195. Enhancement of flame blowout limits by the use of swirl.
7. D. FEIKEMA, R.-H. CHEN and J. F. DRISCOLL 1991 Combustion and Flame 86, 347-358. Blowout of nonpremixed flames: maximum coaxial air velocity achievable, with and without swirl.
8. C. K. W. TAM 1995 Annual Review of Fluid Mechanics 27, 17-23. Supersonic jet noise.
9. E. GUTMARK, K. C. SCHADOW and C. J. BICKER 1990 American Institute of Aeronautics and Astronautics 28, 1163-1170. Near acoustic field and shock structure of rectangular supersonic jets.
10. A. KROTHAPOLLI, Y. HSIA, D. BAGANOFF and K. KARAMCHETI 1986 Journal of Sound and Vibration 106, 119-143. The role of screech tones in mixing of an underexpanded retangular jet.
11. M. BRASSARD, R. H. CHEN and L. CHEW 1996 Journal of Sound and Vibration 197, 255-261. An experimental study of underexpanded square jet noise.
12. E. GUTMARK, K. C. SCHADOW, K. J. WILSON and C. J. BICKER 1988 Physics of Fluids 31, 2524-2532. Near-field pressure radiation and flow characteristics in low supersonic circular and elliptical jets.
13. H. W. LIEPMANN and A. ROSHKO 1957 Elements of Gasdynamics. New York: John Wiley.